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Volumn 96, Issue 1, 1997, Pages 39-44
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Modification of the properties of aircraft engine compressor blades by uninterrupted and pulsed-ion beams
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Author keywords
Ion beam; Refractory alloys; Service properties
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Indexed keywords
ANNEALING;
COATINGS;
COMPOSITION;
COMPRESSORS;
GAS TURBINES;
ION BEAMS;
ION IMPLANTATION;
MATERIALS TESTING;
REFRACTORY ALLOYS;
SURFACE PROPERTIES;
TURBOMACHINE BLADES;
GAS TURBINE ENGINE COMPRESSOR BLADE;
ION BEAM TREATMENT;
PHASE STRUCTURAL STATE;
PHYSICAL CHEMICAL STATE;
SERVICE PROPERTY;
SURFACE TREATMENT;
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EID: 0031551698
PISSN: 02578972
EISSN: None
Source Type: Journal
DOI: 10.1016/s0257-8972(97)00170-9 Document Type: Article |
Times cited : (12)
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References (13)
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